Titlebook: MEGADESIGN and MegaOpt - German Initiatives for Aerodynamic Simulation and Optimization in Aircraft ; Results of the closi Norbert Kroll,Di

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Recent Developments of TAU Adaptation Capabilityect, in particular focusing on advances made in the core of the adaptation module (for example parallel (de-)refinement and other efficiency improvements) as well as a relatively new type of adaptation indicator based on the adjoint solution (among other things) for a goal-oriented mesh adaption..Th

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Efficient Combat Aircraft Simulations with the TAU RANS Codeircraft configurations are mostly dependent on flowfield simulation results with small uncertainty levels. A software package which more and more fulfills those requirements is the TAU Code developed at the DLR over many years. The aim of this contribution is to demonstrate the ability of the TAU co

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Computational Modelling of Transonic Aerodynamic Flows Using Near-Wall, Reynolds Stress Transport Mo-Averaged Navier–Stokes) framework, updated to account for a wall-normal free, non-linear version of the pressure-strain term model, its implementation into the DLR-FLOWer code and its validation in computing some (compressible) transonic flow configurations. Furthermore, the wall boundary condition

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Application of Transition Predictionlichting and cross flow instabilities were coupled for the automatic prediction of laminar-turbulent transition on general three-dimensional aircraft configurations during the ongoing flow computation. In this article, the procedure is applied to a two-dimensional three-element high-lift airfoil con